| タイトル | Retooling CFD for hypersonic aircraft |
| 著者（英） | Kutler, Paul; Povinelli, Louis A.; Dwoyer, Douglas L. |
| 著者所属（英） | NASA Lewis Research Center|NASA Ames Research Center|NASA Langley Research Center |
| 発行日 | 1987-10-01 |
| 言語 | eng |
| 内容記述 | The CFD facility requirements of hypersonic aircraft configuration design development are different from those thus far employed for reentry vehicle design, because (1) the airframe and the propulsion system must be fully integrated to achieve the desired performance; (2) the vehicle must be reusable, with minimum refurbishment requirements between flights; and (3) vehicle performance must be optimized for a wide range of Mach numbers. An evaluation is presently made of flow resolution within shock waves, transition and turbulence phenomenon tractability, chemical reaction modeling, and hypersonic boundary layer transition, with state-of-the-art CFD. |
| NASA分類 | AERONAUTICS (GENERAL) |
| レポートNO | 88A16749 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/373905 |
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